/*--------------------------------*- C++ -*----------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     |
    \\  /    A nd           | Web:      www.OpenFOAM.org
     \\/     M anipulation  |
-------------------------------------------------------------------------------
Description
    Calculates lift, drag and moment coefficients by summing forces on
    specified patches for a case where the solver is compressible (pressure is
    in units M/(LT^2), e.g. Pa).

\*---------------------------------------------------------------------------*/

#include    "$FOAM_CASE/0/U"

patches     (aerofoil);

magUInf     $speed;
lRef        1;
Aref        1; // span
rhoInf      1.2;

CofR        (0.2 0 0);
pitchAxis   (0 1 0);

#includeEtc "caseDicts/functions/forces/forceCoeffs.cfg"

// ************************************************************************* //
